FR2572788B1 - COMPOSITE CARRIER STRUCTURE - Google Patents
COMPOSITE CARRIER STRUCTUREInfo
- Publication number
- FR2572788B1 FR2572788B1 FR8417223A FR8417223A FR2572788B1 FR 2572788 B1 FR2572788 B1 FR 2572788B1 FR 8417223 A FR8417223 A FR 8417223A FR 8417223 A FR8417223 A FR 8417223A FR 2572788 B1 FR2572788 B1 FR 2572788B1
- Authority
- FR
- France
- Prior art keywords
- carrier structure
- composite carrier
- composite
- carrier
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 239000002131 composite material Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D21/00—Understructures, i.e. chassis frame on which a vehicle body may be mounted
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/04—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
- B62D29/041—Understructures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
- B62D29/04—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
- B62D29/048—Connections therefor, e.g. joints
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C23/00—Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
- B66C23/62—Constructional features or details
- B66C23/64—Jibs
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C2/00—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
- E04C2/30—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
- E04C2/34—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
- E04C2/36—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels
- E04C2/365—Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts spaced apart by transversely-placed strip material, e.g. honeycomb panels by honeycomb structures
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/29—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2607/00—Walls, panels
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Civil Engineering (AREA)
- Composite Materials (AREA)
- Laminated Bodies (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8417223A FR2572788B1 (en) | 1984-11-08 | 1984-11-08 | COMPOSITE CARRIER STRUCTURE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8417223A FR2572788B1 (en) | 1984-11-08 | 1984-11-08 | COMPOSITE CARRIER STRUCTURE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2572788A1 FR2572788A1 (en) | 1986-05-09 |
FR2572788B1 true FR2572788B1 (en) | 1987-01-30 |
Family
ID=9309500
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8417223A Expired FR2572788B1 (en) | 1984-11-08 | 1984-11-08 | COMPOSITE CARRIER STRUCTURE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2572788B1 (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0777763B2 (en) * | 1986-05-12 | 1995-08-23 | 川崎重工業株式会社 | Beam-shaped structural members reinforced with fibers |
US4910065A (en) * | 1987-10-15 | 1990-03-20 | The Boeing Company | Reinforced honeycomb core sandwich panels and method for making same |
US5653494A (en) * | 1994-06-29 | 1997-08-05 | Transmaster Technologies Inc. | Modular sport, work, and travel trailer system |
BE1010366A6 (en) * | 1996-06-14 | 1998-07-07 | Groep Stevens Int Nv | Support for a vehicle. |
JPH10264855A (en) * | 1997-03-26 | 1998-10-06 | Aisin Seiki Co Ltd | Vehicle front end modure structure |
FR2772662B1 (en) * | 1997-12-23 | 2000-03-10 | Peugeot | PART OF COMPOSITE MATERIAL WITH EFFORT DISTRIBUTION INSERT, METHOD FOR MANUFACTURING SUCH A PART, MOLD FOR IMPLEMENTING THE METHOD AND ARRANGEMENT FOR APPLYING EFFORTS TO THE PART |
FR2792247A1 (en) * | 1999-04-16 | 2000-10-20 | Fibres De Berre | Composite structure for lining large sewer is polymerized assembly of honeycomb material interlaced with I-shaped pieces of glass fiber fabric and skin covering both ends of fabric pieces |
BE1013229A3 (en) * | 2000-01-13 | 2001-11-06 | Groep Stevens Int Nv | SUPPORT FOR A VEHICLE AND METHOD FOR MANUFACTURING OF SPARS therefor. |
NL1030545C2 (en) * | 2005-11-28 | 2007-05-30 | L Sim B V | Sandwich material for vehicle, has core material that consists of layers of thermoplastic honeycomb material connected by fiber reinforced plastic layers at right angles relative to top layers |
NL1032516C2 (en) * | 2005-11-28 | 2007-06-19 | L Sim B V | Sandwich material. |
FR2902115B1 (en) * | 2006-06-13 | 2008-08-08 | Skf Aerospace France Soc Par A | FIBROUS PIECE FOR COMPOSITE PIECE, COMPOSITE PIECE, AND METHOD FOR MANUFACTURING SUCH A COMPOSITE PIECE |
DE102012215102A1 (en) * | 2012-08-24 | 2014-05-28 | Bayerische Motoren Werke Aktiengesellschaft | Bearing arrangement and axle carrier for a motor vehicle |
FI20146122A (en) * | 2014-12-19 | 2016-06-20 | Konecranes Global Oy | Main beam for a lifting crane |
DE102015104375A1 (en) * | 2015-03-24 | 2016-09-29 | M. Braun Inertgas-Systeme Gmbh | carrier |
DE102020133693B3 (en) * | 2020-12-16 | 2022-06-23 | CG Rail - Chinesisch-Deutsches Forschungs- und Entwicklungszentrum für Bahn- und Verkehrstechnik Dresden GmbH | Transom for a bogie and method for its manufacture |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL284435A (en) * | 1900-01-01 | |||
FR2051877A5 (en) * | 1969-05-30 | 1971-04-09 | Commissariat Energie Atomique | |
DE2327393A1 (en) * | 1972-05-31 | 1973-12-13 | United Aircraft Corp | COMPOSITE HELICOPTER ROTOR BLADE |
US3923421A (en) * | 1974-12-19 | 1975-12-02 | United Technologies Corp | Lightning protected composite helicopter blade |
US4399642A (en) * | 1980-07-24 | 1983-08-23 | The Boeing Company | Aircraft floor panel installation system |
US4335174A (en) * | 1980-09-04 | 1982-06-15 | The Boeing Company | Honeycomb structure end closure |
WO1983001238A1 (en) * | 1981-09-30 | 1983-04-14 | Whitener, Philip, Charles | Composite structural skin spar joint and method of making |
-
1984
- 1984-11-08 FR FR8417223A patent/FR2572788B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2572788A1 (en) | 1986-05-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
ST | Notification of lapse |